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航空用钛合金表面处理工艺参数优化

孙振起 黄明辉 刘昌发

郑州大学学报(工学版)2012,Vol.33Issue(2):125-128,4.
郑州大学学报(工学版)2012,Vol.33Issue(2):125-128,4.DOI:10.3969/j.issn.1671-6833.2012.02.030

航空用钛合金表面处理工艺参数优化

Optimization of Titanium Alloy Surface Anodic Treatment Parameters

孙振起 1黄明辉 1刘昌发1

作者信息

  • 1. 中南大学机电学院,湖南长沙410083
  • 折叠

摘要

Abstract

Ti-6A1-4V is an important alloy in aviation field. In this paper, orthogonal experiment method was used to optimize the parameters of surface treatment, which affect the results of the anodization. The best parameters were obtained with this method; 250 g/L of solution concentration, 10 V electric voltage and 15 minutes anodization time, 25 t experimental temperature. Brown, tight and porous oxide layer was developed on the surface of titanium alloy. This oxide layer increased the surface of the sampld, and enlarged the in-termeshing strength between the cohesive and sample during bonding. Mechanical test results showed that the cohesive joint shear strength comes up to 34.54 Mpa according to this optimized program.

关键词

钛合金/阳极化表面处理/正交实验法/工艺参数优化

Key words

titanium alloy/ anodization surface treatment/ orthogonal experiment/ process parameters optimia-tion

分类

航空航天

引用本文复制引用

孙振起,黄明辉,刘昌发..航空用钛合金表面处理工艺参数优化[J].郑州大学学报(工学版),2012,33(2):125-128,4.

郑州大学学报(工学版)

OA北大核心CSTPCD

1671-6833

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